Air cycle machine bypass duct

Patent metadata

Field	Value
Publication number	US-12110900-B2
Application number	US-202318095835-A
Country	US
Kind code	B2
Filing date	Jan 11, 2023
Priority date	Jan 11, 2023
Publication date	Oct 8, 2024
Grant date	Oct 8, 2024

Abstract

An environmental control system includes a rotary machine, a first bypass duct, and a first check valve in the first bypass duct. The rotary machine includes a compressor section and a first turbine section. Each section of the rotary machine includes an inlet, an outlet, a duct extending between the inlet and the outlet, and an impeller in the duct. The rotary machine also includes a tie rod mechanically connecting the compressor impeller and the first turbine impeller. The first bypass duct is between the compressor section and the first turbine inlet. The check valve opens the first bypass duct when an air pressure in the compressor inlet is higher than an air pressure in the first turbine inlet.

First claim

The invention claimed is:

1. An environmental control system comprising:
a rotary machine comprising:
a compressor section comprising:
a compressor inlet;
a compressor outlet;
a compressor duct extending between the compressor inlet and the compressor outlet; and
a compressor impeller positioned in the compressor duct;

a first turbine section comprising:
a first turbine inlet downstream from the compressor outlet;
a first turbine outlet;
a first turbine duct extending between the first turbine inlet and the first turbine outlet; and
a first turbine impeller positioned in the first turbine duct;

a second turbine section comprising:
a second turbine inlet downstream from the first turbine outlet;
a second turbine outlet;
a second turbine duct extending between the second turbine inlet and the second turbine outlet; and
a second turbine impeller positioned in the second turbine duct and mechanically connected to the tie rod of the rotary machine; and

a tie rod mechanically connecting the compressor impeller and the first turbine impeller;

a first bypass duct between the compressor inlet and the first turbine inlet;
a first check valve in the first bypass duct, wherein the first check valve opens the first bypass duct when the pressure in the compressor inlet is higher than a pressure in the first turbine inlet;
a second bypass duct between the first turbine inlet and the second turbine inlet; and
a second check valve in the second bypass duct, wherein the second check valve opens the second bypass duct when an air pressure in the first turbine inlet is higher than an air pressure in the second turbine inlet.

2. The environmental control system of claim 1 , and further comprising:
a plurality of heat exchangers between the compressor outlet and the first turbine inlet; and
wherein the first bypass duct diverts airflow from the plurality of heat exchangers to the first turbine inlet.

3. The environmental control system of claim 2 , wherein the plurality of heat exchangers comprises:
a first heat exchanger downstream from the compressor outlet;
a second heat exchanger downstream from the first heat exchanger; and
a third heat exchanger downstream from the second heat exchanger.

4. The environmental control system of claim 1 , and further comprising:
a water condenser between the first turbine outlet and the second turbine inlet; and
wherein the second bypass duct diverts airflow from the water condenser to the second turbine inlet.

5. The environmental control system of claim 4 , and further comprising:
a heat exchanger between the first turbine outlet and the second turbine inlet; and
wherein the second bypass duct diverts airflow from the heat exchanger to the second turbine inlet.

6. The environmental control system of claim 5 , wherein the water condenser is upstream from the heat exchanger.

7. The environmental control system of claim 1 , wherein the first check valve and the second check valve are chosen from the group consisting of ball check valves, spring-loaded ball check valves, flapper check valves, spring-loaded flapper check valves, seated check valves, and spring-loaded flapper check valves.

8. The environmental control system of claim 1 , and further comprising:
a heat exchanger downstream from the second turbine section of the rotary machine.

9. The environmental control system of claim 1 , and further comprising:
a fan duct heat exchanger upstream from the compressor inlet.

10. The environmental control system of claim 1 , wherein the rotary machine is downstream from a gas turbine engine bleed air source.

11. The environmental control system of claim 1 , and further comprising:
a plurality of heat exchangers between the compressor outlet and the first turbine inlet;
wherein the first bypass duct diverts airflow from the plurality of heat exchangers when the check valve is open.

12. An environmental control system comprising:
a rotary machine comprising:
a compressor section comprising:
a compressor inlet;
a compressor outlet;
a compressor duct extending between the compressor inlet and the compressor outlet; and
a compressor impeller positioned in the compressor duct;

a turbine section comprising:
a turbine inlet downstream from the compressor outlet of the compressor section;
a turbine outlet;
a turbine duct extending between the turbine inlet and the turbine outlet; and
a turbine impeller positioned in the turbine duct;

a second turbine section comprising:
a second turbine inlet downstream from the turbine outlet;
a second turbine outlet;
a second turbine duct extending between the second turbine inlet and the second turbine outlet; and
a second turbine impeller positioned in the second turbine duct; and

a tie rod mechanically connecting the compressor impeller and the turbine impeller;

a bypass duct between the compressor inlet and the turbine;
a check valve in the bypass duct, wherein the check valve opens the bypass duct when a pressure in the compressor inlet is higher than a pressure in the turbine inlet; and
wherein the bypass duct diverts airflow from the compressor section;
a second bypass duct between the turbine inlet and the second turbine inlet; and
a second check valve in the second bypass duct, wherein the second check valve opens the second bypass duct when an air pressure in the turbine inlet is higher than an air pressure in the second turbine inlet.

13. The environmental control system of claim 12 , and further comprising:
a plurality of heat exchangers between the compressor outlet and the turbine inlet;
wherein the bypass duct diverts airflow from the plurality of heat exchangers when the check valve is open.

14. The environmental control system of claim 12 , wherein the check valve is chosen from the group consisting of ball check valves, spring-loaded ball check valves, flapper check valves, spring-loaded flapper check valves, seated check valves, and spring-loaded flapper check valves.

15. The environmental control system of claim 12 , and further comprising:
a fan duct heat exchanger upstream from the compressor inlet of the rotary machine.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Beers Craig M
• Paliulis John H
• Colson Darryl

Classifications

• F05D2260/606

  Bypassing the fluid · CPC title

• F05D2260/213

  by the provision of a heat exchanger within the cooling circuit · CPC title

• F05D2220/34

  in ram-air turbines ("RATS") · CPC title

• B64D2013/0603

  Environmental Control Systems · CPC title

• B64D13/06 Primary

  the air being conditioned (pressurising B64D13/02) · CPC title